Export to Refworks Export to EndNote Email
Report an Issue

Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing

Author:
Murphy, A. W.
Published:
January 1999.
Physical Description:
1 electronic document
Additional Creators:
Lake, R. E. and Wilkerson, C.
Online Version

Availability

I Want It

Finding items...

Restrictions on Access:
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
An unlined reusable filament wound composite cryogenic tank was tested at the Marshall Space Flight Center using LH2 cryogen and pressurization to 320 psig. The tank was fabricated by Phillips Laboratory and Wilson Composite Group, Inc., using an EnTec five-axis filament winder and sand mandrels. The material used was IM7/977-2 (graphite/epoxy).
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19990019399.
NAS 1.15:209039.
M-909.
NASA/TM-1999-209039.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15643458